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You searched for: creator:"Langley Aeronautical Laboratory"
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[texts]Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854698&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research
Downloads: 86
[texts]Effect of powered propellers on the aerodynamic characteristics and the porpoising stability of a dynamic model of a long-range flying boat - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805116&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 85
[texts]Wind-tunnel investigation of the aerodynamic and structural deflection characteristics of the Goodyear inflatoplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003833712&ix=nu&I=0&V=D&pm=1
Keywords: Research aircraft; Aerodynamics--Research
Downloads: 118
[texts]Experimental verification of the rudder-free stability theory for an airplane model equipped with rudders having negative floating tendency and negligible friction - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806635&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 123
[texts]Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805102&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 97
[texts]General solutions of optimum problems in nonstationary flight - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807493&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Flight testing; Aerodynamics--Research
Downloads: 81
[texts]On the flow of a compressible fluid by the hodograph method. I- Unification and extension of present-day results - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613067&ix=nu&I=0&V=D&pm=1
Keywords: Hodograph equations; Compressibility; Aerodynamics, Supersonic
Downloads: 83
[texts]Numerical evaluation of the [epsilon]-integral occurring in the Theodorsen arbitrary-airfoil potential theory - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605363&ix=nu&I=0&V=D&pm=1
Keywords: Conformal mapping; Harmonic analysis; Aeronautics--Research
Downloads: 85
[texts]On the flow of a compressible fluid by the hodograph method.:II,Fundamental set of particular flow solutions of the Chaplygin differential equation - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605272&ix=nu&I=0&V=D&pm=1
Keywords: Hodograph equations; Compressibility; Aerodynamics, Supersonic
Downloads: 127
[texts]Automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003666890&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Ailerons; Aerodynamics
Downloads: 112
[texts]Force tests of a 1/5-scale model of the type GB-5 controllable glide bomb - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003610203&ix=nu&I=0&V=D&pm=1
Keywords: Guided bombs; Aerodynamics--Research
Downloads: 122
[texts]Wind-tunnel investigation of rounded horns and of guards on a horizontal tail surface - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614495&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Tail surfaces; Aerodynamics--Research
Downloads: 73
[texts]Column and plate compressive strengths of aircraft structural materials extruded 75S-T aluminum-alloy - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807482&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Testing; Aerodynamics--Research
Downloads: 117
[texts]Flight investigation of NACA Ds cowlings on the XP-42 airplane.:II,Low-inlet-velocity cowling with axial-flow fan and propeller cuffs - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805098&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Motors--Cowlings; Aerodynamics--Research
Downloads: 134
[texts]Effects of wing and nacelle modifications on drag and wake characteristics of a bomber-type airplane model - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003633521&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Nacelles; Bombers; Aerodynamics--Research
Downloads: 112
[texts]Wind-tunnel investigation of control-surface characteristics.:XXII, Medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.20-airfoil-chord flap on an NACA 0009 airfoil - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804691&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Flaps (Airplanes; Aeronautics--Research
Downloads: 115
[texts]Qualitative measurements of the effective heats of ablation of several materials in supersonic air jets at stagnation temperatures up to 11,000° F - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810791&ix=nu&I=0&V=D&pm=1
Keywords: Ablation (Aerothermodynamics; Supersonic planes; Aerodynamics--Research
Downloads: 99
[texts]Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 3° trim and with a 22 1/2° angle of dead rise - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003594136&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Airplanes--Landing; Aeronautics--Research
Downloads: 83
[texts]NACA impact basin and water landing tests of a float model at various velocities and weights - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804832&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 128
[texts]Determination of desirable lengths of Z- and channel-section columns for local-instability tests - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806705&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 93
[texts]Approximate determination of the power required to move control surfaces as related to control-booster design - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614183&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 99
[texts]NACA mach number warning device for use in flight - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804356&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Aerodynamics
Downloads: 141
[texts]Heat transfer and skin friction for turbulent boundary layers on heated or cooled surfaces at high speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809208&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics--Research; Skin friction (Aerodynamics
Downloads: 127
[texts]Approximate method for estimating the incompressible laminar boundary-layer characteristics on a flat plate in slipping flow - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810747&ix=nu&I=0&V=D&pm=1
Keywords: Laminar boundary layer; Aerodynamics--Research
Downloads: 84
[texts]Effect of compressibility on the hovering performance of two 10-foot-diameter helicopter rotors tested in the Langley full-scale tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834396&ix=nu&I=0&V=D&pm=1
Keywords: Rotors (Helicopters; Aerodynamics--Research
Downloads: 110
[texts]Wind-tunnel tests of dual-rotating propellers with systematic differences in number of blades, blade setting, and rotational speed of front and rear propellers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638089&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 121
[texts]Investigation of methods of supporting single-thickness specimens in a fixture for determination of compressive stress-strain curves - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806564&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 93
[texts]Flight investigation of boundary-layer transition and profile drag of an experimental low-drag wing installed on a fighter-type airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613553&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Control surfaces; Aerofoils; Aerodynamics--Research
Downloads: 105
[texts]Determination of jet-boundary corrections to cowling-flap-outlet pressures by an electrical analogy method - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805105&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Motors--Cowlings; Airplanes--Nacelles; Aerodynamics--Research
Downloads: 96
[texts]Simple method for estimating terminal velocity including effect of compressibility on drag - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638273&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 94
[texts]Wind-tunnel tests of a dual-rotating propeller having one component locked or windmilling - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003594003&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aeronautics
Downloads: 103
[texts]Comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613545&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Airplanes--Control systems; Aerodynamics--Research
Downloads: 79
[texts]Theoretical and experimental dynamic loads for a prismatic float having an angle of dead rise of 22 1/2° - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638573&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes--Hydrodynamics; Aerodynamics--Research
Downloads: 93
[texts]Flight investigation at high speeds of profile drag of wing of a P-47D airplane having production surfaces covered with camouflage paint - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613208&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Fighter planes; Aerodynamics--Research
Downloads: 107
[texts]Effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614166&ix=nu&I=0&V=D&pm=1
Keywords: Yawing (Aerodynamics; Aerodynamics--Research
Downloads: 187
[texts]Flight investigation at high mach numbers of several methods of measuring static pressure on an airplane wing - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613532&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Bombers; Aerodynamics--Research
Downloads: 110
[texts]Static-pressure error of an airspeed installation on an airplane in high-speed dives and pull-outs - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616343&ix=nu&I=0&V=D&pm=1
Keywords: Static pressure probes; Aerodynamics--Research
Downloads: 90
[texts]Spinning of large airplanes - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613597&ix=nu&I=0&V=D&pm=1
Keywords: Bombers; Transport planes; Aerodynamics--Research
Downloads: 151
[texts]Aerodynamic tests of an M-31 bomb in the 8-foot high-speed tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003612647&ix=nu&I=0&V=D&pm=1
Keywords: Projectiles, Aerial; Aerodynamics--Research
Downloads: 73
[texts]Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638560&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings; Aerofoils; Aerodynamics--Research
Downloads: 101
[texts]Effect on stability and control of a pusher propeller behind conventional tail surfaces as determined by tests of a powered model in the free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805344&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 167
[texts]Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834476&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 85
[texts]Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics--Research; Drag (Aerodynamics
Downloads: 185
[texts]Considerations of wake-excited vibratory stress in a pusher propeller - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605293&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Wakes (Aerodynamics
Downloads: 109
[texts]Investigation of effect of sideslip on lateral stability characteristics.: I, circular fuselage with variations in vertical-tail area and tail length with and without horizontal tail surface - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003619649&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Fuselage--Testing; Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 90
[texts]Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614499&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Damping (Mechanics; Aerodynamics--Research
Downloads: 90
[texts]Effect of normal pressure on the critical shear stress of curved sheet - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806243&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 86
[texts]Analysis of available data on the effectiveness of ailerons without exposed overhang balance - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807486&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 133
[texts]Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613603&ix=nu&I=0&V=D&pm=1
Keywords: Stability of airplanes; Bombers; Aerodynamics--Research
Downloads: 96
[texts]Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613074&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Yawing (Aerodynamics
Downloads: 68
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